Effect of Mach number and Reynolds number on a normal shock-wave/turbulent boundary-layer interaction
- 23 July 1979
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Numerical solution of the interaction of a shock wave with a laminar boundary layerPublished by Springer Nature ,2008
- Comparison of multiequation turbulence models for several shock-separated boundary-layer interaction flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Numerical Investigation of Turbulence Models for Shock-Separated Boundary-Layer FlowsAIAA Journal, 1978
- A normal shock-wave turbulent boundary-layer interaction at transonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Transonic flow about a thick circular-arc airfoilPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975